Centrifugal pump with optimized blades

The centrifugal pump design with optimized blade angles and geometric parameters addresses efficiency challenges in electric vehicle cooling systems, achieving high hydraulic and total efficiency.

FR3151360B1Active Publication Date: 2026-03-27VALEO SYST THERMIQUES SAS
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Patent Information

Authority / Receiving Office
FR · FR
Patent Type
Patents
Current Assignee / Owner
Filing Date
2023-07-18
Publication Date
2026-03-27

AI Technical Summary

Technical Problem

Electric vehicle cooling systems face challenges in optimizing hydraulic efficiency of centrifugal pumps due to increased components and the need for higher pump power, necessitating energy-efficient designs to reduce battery drain.

Method used

A centrifugal pump design with blades extending from a central to a peripheral area on the rotor, featuring a deployment angle of 75° to 110°, preferably 102°, and specific geometric parameters to enhance hydraulic efficiency.

Benefits of technology

The optimized blade design achieves maximum hydraulic efficiency and total efficiency of approximately 0.47, with hydraulic efficiency at 0.70, suitable for electric vehicle cooling systems.

✦ Generated by Eureka AI based on patent content.

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Abstract

A centrifugal pump comprising a rotor (110) with a rotational axis (A) and blades distributed (112) on one face of the rotor (110), the blades extending from a central zone (C1) of the rotor to a peripheral zone (C2) of the rotor. Each blade (112) has a chord (K) extending between a blade root forming an inlet point (E), located in the central zone (C1) of the rotor, and a blade tip forming an outlet point (S), located in the peripheral zone (C2) of the rotor. The inlet point (E) and the outlet point (S) form with the center (O) of the rotor a deployment angle (φ) of between 75° and 110°, preferably greater than 90°, or even greater than 95°, more precisely approximately 102°.
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Description

Title of the invention: Optimized vane centric pump Technical field of the invention

[0001] The present invention relates to a centrifugal pump.

[0002] The invention finds particular application in the automotive field, especially for electric vehicles. Technological background

[0003] In electric vehicles, the number of components in the cooling circuits is increasing, which implies a greater loss of hydraulic pressure to compensate than for a thermal engine.

[0004] Furthermore, in electric vehicles, a specific electric motor is provided for driving the hydraulic pump used to circulate the fluid in the cooling circuit, whereas, in internal combustion engines, the pumps in the cooling circuit are driven by means of a belt linked to the output shaft of the internal combustion engine and the energy taken from the belt to operate the pump is often seen as negligible.

[0005] In electric motors, there is therefore a need to optimize the hydraulic efficiency of these electric pumps in order to save energy drawn from the vehicle's batteries, in an environment where the pump power must also be higher. In this context, the applicant has established that there is an advantageous operating point for such optimization, related to a given pump flow rate and pressure.

[0006] In a known manner, a centrifugal hydraulic pump comprises a volute and a rotor comprising a plurality of blades.

[0007] It is also known to size an electric pump according to many geometric parameters of these elements.

[0008] To optimize the hydraulic efficiency of the electric pump at the identified operating point, the inventors noted that a particularly relevant dimensioning parameter of the electric pump is the angular extent of its blades. Summary of the invention

[0009] A centrifugal pump comprising: is therefore proposed. - a rotor with a rotation axis; and - one or more blades distributed on one face of the rotor, the blade(s) extending from a central area of ​​the rotor to a peripheral area of ​​the rotor; the or the blades having a chord extending between a blade root forming an entry point located in the central area of ​​the rotor, and a blade tip forming an exit point located in the peripheral area of ​​the rotor, the entry point and the exit point forming with the axis of rotation of the rotor, in a plane orthogonal to said axis, a deployment angle of between 75° and 110°, preferably greater than 90°, or even greater than 95°, more precisely equal to about 102°.

[0010] Surprisingly, such a deployment angle advantageously optimizes the hydraulic efficiency of the electric pump for an operating point covering broad needs.

[0011] The invention may further include one or more of the following optional features, according to any technically possible combination.

[0012] Each blade is configured so that it has an inlet flow angle between 16° and 22°, preferably equal to 19°, the inlet flow angle being formed between a tangent to the central zone and a tangent to the chord of the blade concerned at the point of entry.

[0013] Each blade is configured so that it has an outlet flow angle between 19° and 25°, preferably equal to 22°, the outlet flow angle being formed between a tangent to the periphery of the rotor and a tangent to the chord of the blade concerned at the outlet point.

[0014] The rotor has an internal radius, defining the central area of ​​the rotor, of between 9 mm and 11 mm, preferably equal to 10 mm.

[0015] The rotor has an external radius, defining the peripheral area of ​​the rotor, between 22 mm and 25 mm, preferably equal to 23.2 mm.

[0016] Each blade has a decreasing wetted height between the entry point and the exit point of the blade.

[0017] Each blade has a wetted height from inlet to inlet point, between 3.6 and 3.8 mm, preferably equal to 3.7 mm.

[0018] Each blade has a wetted height at the exit point, between 2.3 and 2.5 mm, preferably equal to 2.4 mm.

[0019] The chord of each blade extends along a profile defined by a polynomial of at least order 4, in an orthonormal coordinate system included in a plane orthogonal to said axis of rotation of the rotor and centered on said axis of the rotor, the x-axis of the coordinate system passing through the nose and the y-axis of the coordinate system passing through the root of the blade concerned.

[0020] The polynomial is defined by the following equation: y = -4.10^+1.1.10^3 - 4.4^10.806, where x and y denote the two-dimensional coordinates in the orthonormal frame, such that x is between -3 and 24 mm.

[0021] The pump has a number of blades between 5 and 10, preferably equal to 8.

[0022] Each blade has a thickness between 0.8 and 2 mm, preferably equal to 1 mm. Brief description of the figures

[0023] The invention will be better understood with the aid of the following description, given solely by way of example and made with reference to the accompanying drawings in which: - [Fig.1] illustrates a centrifugal pump according to a particular embodiment of the invention in a top view 1a and a perspective view 1b from a diametrical cutting plane; - [Fig.2] illustrates a sub-assembly of the centrifugal pump according to [Fig.1] according to a side view 2a showing the assembly of a rotor and a flange of said pump, a top view 2b of the rotor and a bottom view 2c of the flange; - [Fig.3] is a top view of part of the pump rotor according to the invention; - [Fig.4] corresponds to [Fig.3] on which is superimposed an example of a 4th order polynomial following a blade; - [Fig.5] is a three-dimensional exploded view of the subset of [Fig.2]; - Figures 6 and 7 illustrate performance results of the centrifugal pump according to the invention. Detailed description of the invention

[0024] A centrifugal pump according to a particular embodiment of the invention will now be described with reference to [Fig.1].

[0025] The centrifugal pump 100 comprises a rotor 110, a fluid inlet flange 120 configured to come opposite the rotor, and an outlet volute 140. The volute has a straight section increasing angularly up to an outlet conduit 150 of said pump.

[0026] Preferably, the rotor 110 is disc-shaped including an opening for the passage of a drive shaft (not shown).

[0027] Preferably, the flange 120 is annular in shape with a central flare. The flange 120 includes a fluid passage orifice 124 located in a central area of ​​the flange 120 and intended to receive an inlet conduit 130 of said pump 100.

[0028] The flange 120 here has a fluid inlet channel connected to a flat area 125 of the flange by a curved area 126. The inlet channel is located at center in axial continuity of the inlet duct 130 and the flat zone 125 is located at the periphery.

[0029] The rotor 110 and the flange 120 will now be described in more detail with reference to [Fig.2].

[0030] The rotor 110 has a rotation axis A corresponding in a plane orthogonal to said axis to a center of rotation O, around which the rotor is intended to be driven by the drive shaft.

[0031] As illustrated in view 2b, the rotor 110 comprises a plurality of blades 112 distributed on one face of the rotor. The rotor 110 and the flange 120 thus define a plurality of passages for the fluid between two adjacent blades.

[0032] Preferably, the number of blades is equal to 8. More generally, this number is between 5 and 10.

[0033] For example, the blades 112 are distributed uniformly, that is to say regularly distributed, angularly, around the axis of rotation of the pump.

[0034] Each blade 112 extends from a central area Cl of the rotor 110 to a peripheral area C2 of the rotor, more particularly, to a peripheral edge C2 of the rotor 110.

[0035] A diameter of the inlet channel of the flange 120 described in Figure 1b is less than a diameter of the central zone Cl of the rotor 110. An external diameter of the curved zone 126 according to Figure 1b is greater than the diameter of the central zone CL. The central part of the rotor 110 is thus located opposite the curved part 126 of the flange 120.

[0036] The flange 120 shown in view 2c has grooves 122 configured to accommodate a longitudinal edge of the blades 112 when the flange 120 is mounted on the rotor 110 as illustrated on the left in view 2a.

[0037] The configuration of the blades 112 will now be described in more detail with reference to [Fig.3].

[0038] The rotor 110 has an inner radius RI defined with respect to the center of rotation O of the rotor 110. Thus, the central area Cl of the rotor is defined by an inner circle centered on the center of rotation O and with a radius equal to the inner radius RL. Preferably, the inner radius RI is equal to 10 mm. More generally, this radius RI is between 9 mm and 11 mm.

[0039] The rotor 110 is provided with an outer edge having an outer radius R2 defined with respect to the center of rotation O of the rotor 110. Thus, the peripheral area C2 of the rotor is defined by an outer circle centered on the center of rotation O and with a radius equal to the outer radius R2. Preferably, the outer radius R2 is equal to 23.2 mm. More generally, this radius R2 is between 22 mm and 25 mm.

[0040] Preferably, each blade 112 has a thickness t equal to 1 mm. More generally, the thickness t is between 0.8 and 2 mm.

[0041] Each blade 112 has a chord K extending between a blade root forming an entry point E located in the central area Cl of the rotor and a blade nose forming an exit point S, located in the peripheral area C2 of the rotor.

[0042] For example, for each blade 112, the entry point E corresponds to the intersection between the chord K and the inner surface of the rotor defined by the inner radius RI. For example, the exit point S corresponds to the intersection between the chord K and the outer surface of the rotor defined by the outer radius R2.

[0043] By definition, the chord of a blade refers to a curve following the profile of the blade from the blade root to the blade tip, so that each point of the curve is equidistant from the walls of the blade.

[0044] The blades have a curved profile between their blade root and their blade nose.

[0045] According to a particular feature of the invention, the entry point E and the exit point S form, with the center O of the rotor, a deployment angle q> of between 75° and 110°, preferably greater than 90°, or even greater than 95°. In the present example, the deployment angle q> is approximately 102°.

[0046] For each blade 112, an inlet flow angle

[31] is defined at the level of the blade root formed between the tangent Tl' to the internal circle Cl of internal radius RI of the rotor 110 and the tangent Tl to the chord K of the blade concerned at the inlet point E.

[0047] Preferably, the inlet flow angle

[31] is approximately 19°. More generally, this angle

[31] is between 16° and 22°.

[0048] For each blade 112, an outlet flow angle

[32] is defined at the level of the blade nose, formed between the tangent T2' to the periphery C2 of the rotor 110 and the tangent T2 to the chord K of the blade concerned at the outlet point S.

[0049] Preferably, the outlet flow angle

[32] is approximately 22°. More generally, this angle is between 19° and 25°.

[0050] All the entry points E of the blades 112 are arranged at equidistant intervals in pairs, preferably along the internal circle Cl of internal radius RI and the blades all have the same chord profile, so that, as already mentioned, the blades are uniformly distributed on the face of the rotor 110.

[0051] An example of a blade chord will now be described with reference to [Fig.4] which reproduces [Fig.3].

[0052] To define the chord K of this blade 112, a reference orthonormal frame (X,Y) is first defined, lying in a plane orthogonal to the axis of rotation of the rotor 110. This frame (X,Y) is centered on the center of rotation O of the rotor 110 in this plane. In other words, the origin (X=0, Y=0) of the frame coincides with the center of rotation O. This frame is oriented such that the abscissa axis X of the frame passes through the nose of blade 112 and the Y axis of the coordinate system passes through the base of blade 112 (specifically an intrados of the base of the blade in question).

[0053] Preferably, the chord K of the blade 112 extends along a profile defined by a fourth-order polynomial, defined in the orthonormal coordinate system (X,Y) by the following equation: y = -4.10^+1,L10'3^3-4.45.10'2x2-0.486Lx+10.806, where x and y denote the two-dimensional coordinates in the orthonormal coordinate system, such that x is between -3 and 24 mm. The correlation coefficient R2, used to assess the accuracy of this estimate, is 0.9994.

[0054] In the present example, all the other blades 112 have a chord defined by the same polynomial by rotation of the orthonormal frame (X,Y) around the axis of rotation O. In other words, each blade 112 has the same profile.

[0055] The height profile of the blades 112 will now be described with reference to [Fig.5], which is an exploded perspective view of the assembly formed by the rotor 110 and the flange 120.

[0056] Preferably, each blade 112 has a wetted inlet height bl at the inlet point E equal to 3.7 mm. More generally, this height b1 is between 3.6 and 3.8 mm.

[0057] Preferably, each blade 112 has a wetted height b2 at the exit point S equal to 2.4 mm. More generally, this height b2 is between 2.3 and 2.5 mm.

[0058] By definition, the wetted height refers to the dimension of the blade in the direction parallel to the axis of rotation of the pump, for the part of the blade immersed in the flow.

[0059] In the present example, the height of each blade 112 varies between its entry point E and its exit point S. Preferably, the wetted height at the inlet bl is slightly higher than the wetted height at the outlet b2, by about 1 / 3.

[0060] Figure 5 shows, in solid lines, an example of a transverse profile P of a blade 112. According to this example, the blade 112 has a constant height of b2 along most of the outer radius R2 of the rotor 110 from its periphery C2, in particular over 80% or even 90% of its chord length, and increases progressively in the central area Cl of the rotor 110 to reach a maximum height at the center O of the rotor 110 equal to bl. This characteristic facilitates a fluid transition between the flange inlet channel and the fluid passages between the blades. After this transition zone, the cross-section of the fluid passages is substantially constant.

[0061] With reference to the figures described above and as already indicated, the blades 112 of the rotor 110 are identical, i.e., they all have the same chord defined by a polynomial and the same height profile. However, in other embodiments, the blades will not necessarily all be identical.

[0062]

[0063]

[0064]

[0065]

[0066]

[0067]

[0068]

[0069] The performance of the centrifugal pump as described above has been evaluated in terms of efficiency from measurement results which will now be described with reference to [Fig.6]. By definition, the total efficiency q of a centrifugal pump is the product of the hydraulic efficiency qh and the mechanical efficiency qm, as defined by the following equation: [Math. 1] : x _ &L - _ t with jx nm - IxU, or ~Cxw and ~IxU Q: volumetric flow rate (in L / h); P: pressure (mbar) C: torque (Nm) U: voltage (V) I: current (A) co: rotational speed (rad / s) For the centrifugal pump 100 as described above, [Fig. 6] represents the volumetric flow rate Q expressed in L / h on the x-axis: - on a GP curve, the pressure P expressed in mbar on the ordinates; - on a Gnh curve, the hydraulic efficiency on the ordinates; and - on a curve Gn, the total yield on the ordinates. These curves were obtained by measurement when the centrifugal pump 100 is configured at an operating point F for which the rotational speed co of the rotor 110 is maintained at 7300 revolutions per minute (rpm). For this operating point, the total efficiency q is found to be at its maximum, approximately equal to 0.47, while the hydraulic efficiency qh is also at its maximum, approximately equal to 0.70. Figure 7 illustrates the performance of an electric motor configured to drive the centrifugal pump 100 according to the invention used to circulate the cooling circuit fluid in an electric vehicle, when the pump is configured at the operating point F described with reference to Figure 5. The performance of the electric motor was measured in terms of electrical power and torque. The results of these measurements are represented, as a function of the volumetric flow rate Q expressed in L / h on the x-axis, - by a curve GPere representing the electrical power Pe expressed in W on the ordinates; and - by a curve Gcre representing the torque C expressed in Nm. By definition, electrical power Pe is defined by the product of an electrical voltage U and an electrical current I.

[0070] According to these results, it can be seen that for a volumetric flow rate corresponding to the predefined operating point F, i.e. Q approximately equal to 2300 L / h, the torque and electrical power have almost reached their maximum value.

Claims

Demands

1. Centrifugal hydraulic pump (100) comprising: - a rotor (110) with an axis of rotation (A); - one or more blades distributed (112) on one face of the rotor, the blade(s) extending from a central zone (Cl) of the rotor to a peripheral zone (C2) of the rotor; the blade(s) having a chord (K) extending between a blade root forming an entry point (E), located in the central zone (Cl) of the rotor, and a blade tip forming an exit point (S), located in the peripheral zone (C2) of the rotor;the entry point (E) and the exit point (S) forming with the axis of rotation (A) of the rotor, in a plane orthogonal to said axis (A), a deployment angle (q>) between 75° and 110°, preferably greater than 90°, or even greater than 95°, more precisely equal to about 102°, the centrifugal hydraulic pump (100) being characterized in that the chord (K) of each blade (112) extends according to a profile defined by a polynomial of order 4, in an orthonormal frame (X,Y) included in a plane orthogonal to said axis of rotation (A) of the rotor and centered on said axis of the rotor, the abscissa axis (X) of the frame passing through the nose (S) and the ordinate axis (Y) of the frame passing through the root (E) of the blade concerned (112), the polynomial being defined by the following equation: y=-4. ¢102 A(-5).xA4+1.

1. ¢102 A(-3).xA3-4.

45. ¢102 A(-2) xA2-0.4861.x+10.806, where x and y denote the two-dimensional coordinates in the orthonormal frame (X,Y), such that x is between -3 and 24 mm.;

2. Pump according to claim 1, wherein each blade (112) is configured so that it has an inlet flow angle ([31] between 16° and 22°, preferably equal to 19°, the inlet flow angle ([31] being formed between a tangent (TT) to the central zone (Cl) and a tangent (Tl) to the chord (K) of the blade concerned at the inlet point (E).

3. Pump according to claim 1 or 2, wherein each blade (112) is configured such that it has an outlet flow angle ([32]) between 19° and 25°, preferably equal to 22°, the outlet flow angle ([32]) being formed between a tangent (T2') to the periphery (C2) of the rotor and a tangent (T2) to the chord (K) of the blade concerned at the exit point (S).

4. Pump according to any one of claims 1 to 3, wherein the rotor (110) has an internal radius (RI) defining the central zone (Cl), said radius being between 9 mm and 11 mm, preferably equal to 10 mm.

5. Pump according to any one of claims 1 to 4, wherein the rotor (110) has an external radius (R2) defining the peripheral zone (C2), said radius being between 22 mm and 25 mm, preferably equal to 23.2 mm

6. Pump according to any one of claims 1 to 5, wherein each blade (112) has an inlet wetted height (bl) at the inlet point (E) of between 3.6 and 3.8 mm, preferably equal to 3.7 mm.

7. Pump according to any one of claims 1 to 6, wherein each blade (112) has an outlet wetted height (b2) at the outlet point (S) of between 2.3 and 2.5 mm, preferably equal to 2.4 mm.

8. Pump according to any one of claims 1 to 7, wherein the pump has a number of blades between 5 and 10, preferably equal to 8.

9. Pump according to any one of claims 1 to 8, wherein each blade has a thickness of between 0.8 and 2 mm, preferably equal to 1 mm.